2023.1

2023.1

PARAM, SRCOMPS

Bulk Data Entry Outputs the strength ratios for composite elements that have failure indices requested.

Parameter	Values	Description
`SRCOMPS`	<YES, NO, blank>	YES The strength ratios are output for composite elements that have failure indices requested. (The Output formats currently supported are: H3D, HM, OP2, PCH and OPT). NO (Default), blank The strength ratio will not be output.

Comments

The Strength Ratios that are output as a result of PARAM, SRCOMPS, YES depend on the specified Failure Theory. The following equations show the relationship between the Failure Index and the Strength Ratio for different Failure Theories.
- Hill Failure Theory:
  $Strength Ratio = \frac{1}{\sqrt{Failure Index}}$
- Hoffman Failure Theory:
  There is no direct relationship between the Strength Ratio and Failure Index (refer to Composite Laminates in the User Guide for more information). OptiStruct solves the quadratic equation to find the strength ratio.
- Tsai-Wu Failure Theory:
  There is no direct relationship between the Strength Ratio and Failure Index. (refer to Composite Laminates in the User Guide for more information). OptiStruct solves the quadratic equation to find the strength ratio.
- Maximum Stress (Strain) Failure Theory:
  $S t r e n g t h R a t i o = \frac{1}{F a i l u r e I n d e x}$
- Transverse Shear Failure Theory:
  $S t r e n g t h R a t i o = \frac{1}{F a i l u r e I n d e x}$
- Cuntze Failure Theory:
  $S t r e n g t h R a t i o = \frac{1}{F a i l u r e I n d e x}$